{"created":"2023-06-20T14:36:28.748012+00:00","id":2789,"links":{},"metadata":{"_buckets":{"deposit":"c862ae36-c2e9-4306-a3b7-a46e107e0a39"},"_deposit":{"created_by":1,"id":"2789","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"2789"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00002789","sets":["1887:1893","9:1090:1333:1361"]},"author_link":["8970","8969"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Method of simultaneous injection of 3 vehicles into a quasi-zenithal orbit"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2004-03-25","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"14","bibliographicPageStart":"7","bibliographicVolumeNumber":"JAXA-RM-03-004","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構研究開発資料: 準天頂軌道への投入法の検討"},{"bibliographic_title":"JAXA Research and Development Memorandum: Study of Method of Injection into Quasi-Method Orbit","bibliographic_titleLang":"en"}]}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0046957002","subitem_description_type":"Other"}]},"item_3_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: JAXA-RM-03-004","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-1121","subitem_source_identifier_type":"ISSN"}]},"item_3_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA11983593","subitem_source_identifier_type":"NCID"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"宇宙航空研究開発機構 技術研究本部"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Office of Research and Development"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"歌島, 昌由"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Utashima, Masayoshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2020-01-15"}],"displaytype":"detail","filename":"46957002.pdf","filesize":[{"value":"342.5 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"46957002.pdf","url":"https://jaxa.repo.nii.ac.jp/record/2789/files/46957002.pdf"},"version_id":"47523d8c-0565-4ee2-96d4-2086d8ca01ac"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"GTO","subitem_subject_scheme":"Other"},{"subitem_subject":"高速データ通信","subitem_subject_scheme":"Other"},{"subitem_subject":"高精度","subitem_subject_scheme":"Other"},{"subitem_subject":"距離測定","subitem_subject_scheme":"Other"},{"subitem_subject":"静止衛星","subitem_subject_scheme":"Other"},{"subitem_subject":"投入軌道","subitem_subject_scheme":"Other"},{"subitem_subject":"アポジブーストモータ","subitem_subject_scheme":"Other"},{"subitem_subject":"イオンエンジン","subitem_subject_scheme":"Other"},{"subitem_subject":"GTO","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"high speed data communication","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"precision","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"rangefinding","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"synchronous satellite","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transfer orbit","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"apogee boost motor","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"ion engine","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"jpn"}]},"item_resource_type":{"attribute_name":"資源タイプ","attribute_value_mlt":[{"resourcetype":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"準天頂軌道への3機同時投入法","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"準天頂軌道への3機同時投入法"}]},"item_type_id":"3","owner":"1","path":["1361","1893"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"2789","relation_version_is_last":true,"title":["準天頂軌道への3機同時投入法"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T09:16:03.291619+00:00"}